lano I MI di - Aalborg Universitetkom.aau.dk/project/vtcp/wt_sym_2011/slides/CarloLBottasso.pdf ·...
Transcript of lano I MI di - Aalborg Universitetkom.aau.dk/project/vtcp/wt_sym_2011/slides/CarloLBottasso.pdf ·...
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INTEGRATED ACTIVE AND PASSIVE LOAD MITIGATION IN WIND TURBINES
C.L. Bottasso, F. Campagnolo, A. Croce, C. Tibaldi Politecnico di Milano, Italy
Wind Turbine Control Symposium 28-29 November 2011, Ålborg, Denmark
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Need for Load Mitigation
Trends in wind energy:
Increasing wind turbine size ▶
Off-shore wind ▼
To decrease cost of energy:
• Reduce extreme loads
• Reduce fatigue damage
• Limit actuator duty cycle
• Ensure high reliability/availability
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Presentation Outline
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Active Load Mitigation: Pitch Control Individual blade Pitch Control (IPC)
Inner loop (collective pitch): regulation to set point and alleviation of gust loads
Outer loops (individual pitch): reduction of
- Deterministic (periodic) loads due to blade weight and non-uniform inflow
- Non-deterministic loads, caused by fast temporal and small spatial turbulent wind fluctuations
▼ Uniform wind ▼ Turbulent wind
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Active Load Mitigation: Predictive LiDAR-Enabled Pitch Control
LiDAR: generic model, captures realistically wind filtering due to volumetric averaging
Receding Horizon Control: model predictive formulation with wind scheduled linear model, real-time implementation based on CVXGEN
Non-Homogeneous LQR Control: approximation of RHC, extremely low computational cost
LiDAR prediction span
Reduced peak values
Reduced peak values
Reduced peak to peak oscillations
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Flow control devices:
• TE flaps
• Microtabs
• Vortex generators
• Active jets (plasma, synthetic)
• Morphing airfoils
• …
Active Load Mitigation: Distributed Control
(Chow and van Dam 2007)
(Credits: Smart Blade GmbH)
(Credits: Risoe DTU)
(Credits: Risoe DTU)
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Pitch control:
• Limited temporal bandwidth (max pitch rate ≈ 7-9 deg/sec)
• Limited spatial bandwidth (pitching the whole blade is ineffective for spatially small wind fluctuations)
Distributed control:
• Alleviate temporal and spatial bandwidth issues
• Complexity/availability/maintenance
All sensor-enabled control solutions:
• Complexity/availability/maintenance
Active Load Mitigation: Limits and Issues
Off-shore: need to prove reliability, availability, low maintenance in harsh hostile environments
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Presentation Outline
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Passive control: loaded structure deforms so as to reduce load
Two main solutions:
Potential advantages: no actuators, no moving parts, no sensors
(if you do not have them, you cannot break them!)
Other passive control technologies (not discussed here): - Tuned masses (e.g. on off-shore wind turbines to damp nacelle-tower motions)
- Passive flaps/tabs
- …
Passive Load Mitigation
Angle fibers in skin and/or spar caps
- Bend-twist coupling (BTC): exploit anisotropy of composite materials
- Swept (scimitar) blades
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Present study:
• Design BTC blades (all satisfying identical design requirements: max tip deflection, flap freq., stress/strain, fatigue, buckling)
• Consider trade-offs (load reduction/weight increase/complexity)
• Identify optimal BTC blade configuration
• Integrate passive BTC and active IPC
• Exploit synergies between passive and active load control
Baseline uncoupled blade: 45m Class IIIA 2MW HAWT
Objectives
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Presentation Outline
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Optimization-Based Multi-Level Blade Design
Cost: AEP Aerodynamic parameters: chord, twist, airfoils
Cost: Blade weight (or cost model if available) Structural parameters: thickness of shell and spar caps, width and location of shear webs
Cost: AEP/weigh (or cost model if available) Macro parameters: rotor radius, max chord, tapering, …
Controls: model-based (self-adjusting to changing design)
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“F
ine”
level: 3
D F
EM
“Coars
e”
level: 2
D F
EM
secti
on &
beam
models
- Definition of complete HAWT Cp-Lambda multibody model - DLCs simulation - Campbell diagram
DLC post-processing: load envelope, DELs, Markov, max tip deflection
- Definition of geometrically exact beam model - Span-wise interpolation
- ANBA 2D FEM sectional analysis - Computation of 6x6 stiffness matrices
Definition of sectional design parameters
Constraints: - Maximum tip deflection - 2D FEM ANBA analysis of maximum stresses/strains - 2D FEM ANBA fatigue analysis
- Compute cost (mass)
Automatic 3D CAD model generation by lofting of sectional geometry
Automatic 3D FEM meshing (shells and/or solid elements) Update of blade mass (cost)
Analyses: - Max tip deflection - Max stress/strain - Fatigue - Buckling
Verification of design constraints
SQP optimizer
min cost s.t. constraints
Constraint/model update heuristic (to repair constraint violations)
When SQP converged
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The Importance of Multi-Level Blade Design
Stress/strain/fatigue: - Fatigue constraint not satisfied at
first iteration on 3D FEM model - Modify constraint based on 3D
FEM analysis - Converged at 2nd iteration
Fatigue damage constraint satisfied
Buckling: - Buckling constraint not satisfied at first iteration - Update skin core thickness - Update trailing edge reinforcement strip - Converged at 2nd iteration
Peak stress on initial model
Increased trailing edge strip
ITERATION 1 ITERATION 0
ITERATION 1 ITERATION 0
ITERATION 1 ITERATION 0
ITERATION 1 ITERATION 0
No
rmalized s
tress
F
ati
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am
age in
dex
T
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T
railin
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trip
th
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Increased skin core thickness
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2MW 45m Wind Turbine Blade Currently undergoing certification at TÜV SÜD
CNC machined model of aluminum alloy for visual inspection of blade shape
Design developed in partnership with Gurit (UK)
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Presentation Outline
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Fully Coupled Blades
1. Identify optimal section-wise fiber rotation
Consider 6 candidate configurations
BTC coupling parameter:
𝜶 =𝑲𝑩𝑻
𝑲𝑩𝑲𝑻
Spar-cap angle
Skin angle
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Fully Coupled Blades: Effects on Weight
Spar-caps: steep increase
Skin: milder increase
Spar-cap/skin synergy
Stiffness driven design (flap freq. and max tip deflection constraints):
Need to restore stiffness by increasing spar/skin thickness
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Fully Coupled Blades: Load Reduction Spar-cap/skin synergy: good
load reduction with small mass increase
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Fully Coupled Blades: Mechanism of Load Reduction
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Fully Coupled Blades: Effects on Duty Cycle
◀ Less pitching from active control because blade passively self-unloads
Much reduced life-time ADC ▶
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Partially Coupled Blades
2. Identify optimal span-wise fiber rotation: 5 candidate configurations
Reduce fatigue in max chord region
Avoid thickness increase to satisfy stiffness-driven
constraints
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Partially Coupled Blades: Effects on Mass
Too little coupling
Fully coupled blade
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Partially Coupled Blades: Effects on Loads
F30: load reduction close to fully coupled case
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Partially Coupled Blades: Effects on Duty Cycle
Best compromise: similar load and ADC reduction as fully coupled blade, decreased mass
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Integrated Passive and Active Load Alleviation
Individual blade pitch controller (Bossaniy 2003):
• Coleman transform blade root loads
• PID control for transformed d-q loads
• Back-Coleman-transform to get pitch inputs
Baseline controller: MIMO LQR
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Integrated Passive and Active Load Alleviation
Two IPC gain settings:
1. Mild: some load reduction, limited ADC increase
2. Aggressive: more load reduction, more ADC increase
Five blade/controller combinations:
• BTC: best coupled blade + collective LQR
• IPC1: uncoupled blade + mild IPC
• BTC+IPC1: best coupled blade + mild IPC
• IPC2: uncoupled blade + aggressive IPC
• BTC+IPC2: best coupled blade + aggressive IPC
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Integrated Passive/Active Control: Effects on Loads
▲ Synergistic effects of combined passive and
active control ▶
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Integrated Passive/Active Control: Effects on Duty Cycle
Not significant: ADC very small here
Same ADC as baseline (but great load reduction!)
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• Optimization-based blade design tools: enable automated design of
blades and satisfaction of all desired design requirements
• BTC passive load control: - Skin fiber rotation helps limiting spar-cap fiber angle - Partial span-wise coupling limits fatigue and stiffness effects Reduction for all quality metrics: loads, ADC, weight
• Combined BTC/IPC passive/active control: - Synergistic effects on load reduction - BTC helps limiting ADC increase due to IPC (e.g., could have same
ADC as baseline blade with collective pitch control)
Outlook: • Manufacturing implications of BTC and partially coupled blades • Passive distributed control and integration with blade design and
active IPC control
Conclusions
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Outlook: Testing with (WT)2, the Wind Turbine in the Wind Tunnel
Applications: • Testing of advanced control laws and supporting technologies • Testing of extreme operating conditions • Tuning of mathematical models • Aeroelasticity and system identification of wind turbines • Multiple wind turbine interactions • Off-shore wind turbines (moving platform actuated by hydro-structural model)
Conical spiral gears
Main shaft with torque meter
Pitch actuator electronics
Slip ring
Torque actuator: • Planetary gearhead • Torque and speed control
Pitch actuator: • Zero backlash gearhead • Built-in encoder
Rotor sensor electronics
4x3.8m, 55m/s, aeronautical section: • Turbulence <0.1% • Open-closed test section
13.8x3.8m, 14m/s, civil section: • Turbulence < 2% • With turbulence generators = 25% • 13m turntable
Civil-Aeronautical Wind Tunnel of the Politecnico di Milano
Aeroelastically scaled blades
(70g, 1m)
▶ Aeroelastically-scaled wind tunnel model of the Vestas V90 wind turbine with individual blade pitch and torque control
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Turbulence (boundary layer) generators
Outlook: Testing with (WT)2, the Wind Turbine in the Wind Tunnel
Good aerodynamic performance even at low Reynolds ▶
Blockage correction verified by RANS CFD
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Real-time PC running mathematical model of wet part of offshore machine (hydro-elastic model)
WT response
Platform motion
6 DOF moving platform
Outlook: Off-Shore Aero-Elastic Model
Applications: • Testing of control laws • Damping enhancement controllers • Load-reducing controllers • Floating platform effects on stability
▶ Goal: aeroelastically-scaled wind tunnel model of off-shore wind turbine with individual blade pitch and torque control
Proof of concept, 2 DOF hydraulic actuation (prescribed)
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Acknowledgements
Thanks to the POLI-Wind team!
Special thanks to M. Bassetti, P. Bettini, M. Biava, F. Campagnolo, S. Calovi, S. Cacciola, F. Cadei, G. Campanardi, M. Capponi, A. Croce, G. Galetto, L. Maffenini, P. Marrone, M. Mauri, S. Rota, G. Sala, A. Zasso of the Politecnico di Milano
Funding provided by Vestas Wind Systems A/S, Clipper Windpower, Alstom Wind, Italian Ministry of Education, University and Research